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美国政府科技报告
>Wind-tunnel investigation at high subsonic speeds of the static longitudinal and static lateral stability characteristics of a wing-fuselage combination having a triangular wing of aspect ratio 2.31 and an NACA 65A003 airfoil
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Wind-tunnel investigation at high subsonic speeds of the static longitudinal and static lateral stability characteristics of a wing-fuselage combination having a triangular wing of aspect ratio 2.31 and an NACA 65A003 airfoil